I have been trying to model the pitching dynamics of a General Aircraft (Nelson : Flight Stability and Control) but during the modelling, I find that I need to use the Zδe which uses CZδe parameter, in the control matrix B but no where in Nelson a method has been provided to find it. Your help will be appreciated as I need to complete my work on an urgent basis.
I am attaching a picture of the state space equations for your reference.
Thank You]1]2